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1. 发明申请

US20100297472A1 OXIDATION-CORROSION RESISTANT COATING 有权
标题翻译：氧化 - 耐腐蚀涂料
公开(公告)号：US20100297472A1
公开(公告)日：2010-11-25
申请号：US12470993
申请日：2009-05-22
申请人： Michael Minor , Paul M. Pellet , Michael L. Miller , Brian S. Tryon
发明人： Michael Minor , Paul M. Pellet , Michael L. Miller , Brian S. Tryon
IPC分类号： B32B15/01 , C23C16/44 , C22C19/05
CPC分类号： C23C30/00 , C23C4/073 , C23C14/16 , Y10T428/12778 , Y10T428/12944
摘要： A metallic coating for protecting a substrate from high temperature oxidation and hot corrosion environments comprising about 2.5 to about 13.5 wt. % cobalt, about 12 to about 27 wt. % chromium, about 5 to about 7 wt. % aluminum, about 0.0 to about 1.0 wt. % yttrium, about 0.0 to about 1.0 wt. % hafnium, about 1.0 to about 3.0 wt. % silicon, about 0.0 to about 4.5 wt. % tantalum, about 0.0 to about 6.5 wt. % tungsten, about 0.0 to about 2.0 wt. % rhenium, about 0.0 to about 1.0 wt. % molybdenum and the balance nickel.
摘要翻译：用于保护基材免受高温氧化和热腐蚀环境的金属涂层，其包含约2.5至约13.5wt。％钴，约12至约27wt。约5至约7wt。％的铬。％铝，约0.0至约1.0wt。％钇，约0.0至约1.0wt。％铪，约1.0至约3.0wt。％硅，约0.0-约4.5wt。％钽，约0.0-约6.5wt。％钨，约0.0至约2.0重量％％铼，约0.0至约1.0wt。钼和余量为镍。

2. 发明授权

US08354176B2 Oxidation-corrosion resistant coating 有权
标题翻译：耐氧化涂层
公开(公告)号：US08354176B2
公开(公告)日：2013-01-15
申请号：US12470993
申请日：2009-05-22
申请人： Michael Minor , Paul M. Pellet , Michael L. Miller , Brian S. Tryon
发明人： Michael Minor , Paul M. Pellet , Michael L. Miller , Brian S. Tryon
IPC分类号： B32B15/00 , C22C19/05
CPC分类号： C23C30/00 , C23C4/073 , C23C14/16 , Y10T428/12778 , Y10T428/12944
摘要： A metallic coating for protecting a substrate from high temperature oxidation and hot corrosion environments comprising about 2.5 to about 13.5 wt. % cobalt, about 12 to about 27 wt. % chromium, about 5 to about 7 wt. % aluminum, about 0.0 to about 1.0 wt. % yttrium, about 0.0 to about 1.0 wt. % hafnium, about 1.0 to about 3.0 wt. % silicon, about 0.0 to about 4.5 wt. % tantalum, about 0.0 to about 6.5 wt. % tungsten, about 0.0 to about 2.0 wt. % rhenium, about 0.0 to about 1.0 wt. % molybdenum and the balance nickel.
摘要翻译：用于保护基材免受高温氧化和热腐蚀环境的金属涂层，其包含约2.5至约13.5wt。％钴，约12至约27wt。约5至约7wt。％的铬。％铝，约0.0至约1.0wt。％钇，约0.0至约1.0wt。％铪，约1.0至约3.0wt。％硅，约0.0-约4.5wt。％钽，约0.0-约6.5wt。％钨，约0.0至约2.0重量％％铼，约0.0至约1.0wt。钼和余量为镍。

3. 发明授权

US08366386B2 Method and assembly for gas turbine engine airfoils with protective coating 有权
标题翻译：具有保护涂层的燃气涡轮发动机翼型的方法和装配
公开(公告)号：US08366386B2
公开(公告)日：2013-02-05
申请号：US12360312
申请日：2009-01-27
申请人： Daniel E. Quinn , David J. Hiskes , Carl W. Mercier , Michael Minor , Paul M. Pellet , Michael L. Miller
发明人： Daniel E. Quinn , David J. Hiskes , Carl W. Mercier , Michael Minor , Paul M. Pellet , Michael L. Miller
IPC分类号： F04D29/44
CPC分类号： F01D9/02 , F01D5/288 , F05D2230/237 , F05D2230/90 , Y02T50/67 , Y10T29/49231 , Y10T29/49238
摘要： A method of processing turbine airfoils includes depositing a protective coating on first and second turbine airfoils, and bonding the first and second turbine airfoils together after the deposition such that there is an open throat between the first and second turbine airfoil and at least portions of surfaces in the open throat are coated with the protective coating.
摘要翻译：一种处理涡轮机翼片的方法包括在第一和第二涡轮机翼型上沉积保护涂层，以及在沉积之后将第一和第二涡轮机翼型件结合在一起，使得在第一和第二涡轮机翼面之间存在开放的喉部和至少部分表面在开放的喉咙里涂上保护涂层。

4. 发明授权

US08075662B2 Nickel braze alloy composition 有权
标题翻译：镍钎焊合金组成
公开(公告)号：US08075662B2
公开(公告)日：2011-12-13
申请号：US12109398
申请日：2008-04-25
申请人： Michael Minor , Paul M. Pellet , Michael L. Miller
发明人： Michael Minor , Paul M. Pellet , Michael L. Miller
IPC分类号： B22F1/00
CPC分类号： C22C19/057 , B23K35/304 , B23K2101/001 , C22C1/0433 , C22C19/055 , C22C19/056
摘要： A nickel braze alloy composition includes a blend of a first nickel alloy and a second nickel alloy. The first nickel alloy includes about 4.75 wt %-10.5 wt % of chromium, about 5.5 wt %-6.7 wt % of aluminum, up to about 13 wt % cobalt, about 3.75 wt %-9.0 wt % of tantalum, about 1.3 wt %-2.25 wt % of molybdenum, about 3.0 wt %-6.8 wt % of tungsten, about 2.6 wt %-3.25 wt % of rhenium, up to about 0.02 wt % of boron, about 0.05 wt %-2.0 wt % of hafnium, up to about 0.14 wt % of carbon, up to about 0.35 wt % of zirconium, and a balance of nickel. The second nickel alloy includes about 21.25 wt %-22.75 wt % of chromium, about 5.7 wt %-6.3 wt % of aluminum, about 11.5 wt %-12.5 wt % of cobalt, about 5.7 wt %-6.3 wt % of silicon, boron in an amount no greater than 1.0 wt %, and a balance of nickel.
摘要翻译：镍钎焊合金组合物包括第一镍合金和第二镍合金的共混物。第一种镍合金包括约4.75wt％-10.5wt％的铬，约5.5wt％-6.7wt％的铝，至多约13wt％的钴，约3.75wt％的-9.0wt％的钽，约1.3wt％ -2.25重量％的钼，约3.0重量％的-6.8重量％的钨，约2.6重量％的-3.25重量％的铼，至多约0.02重量％的硼，约0.05重量％〜2.0重量％的铪，至约0.14重量％的碳，至多约0.35重量％的锆，余量为镍。第二镍合金包括约21.25重量％-22.75重量％的铬，约5.7重量％-6.3重量％的铝，约11.5重量％-12.5重量％的钴，约5.7重量％-6.3重量％的硅，硼不大于1.0重量％，余量为镍。

5. 发明申请

US20100189555A1 METHOD AND ASSEMBLY FOR GAS TURBINE ENGINE AIRFOILS WITH PROTECTIVE COATING 有权
标题翻译：具有保护涂层的气体涡轮发动机空气的方法和装配
公开(公告)号：US20100189555A1
公开(公告)日：2010-07-29
申请号：US12360312
申请日：2009-01-27
申请人： Daniel E. Quinn , David J. Hiskes , Carl W. Mercier , Michael Minor , Paul M. Pellet , Michael L. Miller
发明人： Daniel E. Quinn , David J. Hiskes , Carl W. Mercier , Michael Minor , Paul M. Pellet , Michael L. Miller
IPC分类号： F01D9/02 , C23C16/22
CPC分类号： F01D9/02 , F01D5/288 , F05D2230/237 , F05D2230/90 , Y02T50/67 , Y10T29/49231 , Y10T29/49238
摘要： A method of processing turbine airfoils includes depositing a protective coating on first and second turbine airfoils, and bonding the first and second turbine airfoils together after the deposition such that there is an open throat between the first and second turbine airfoil and at least portions of surfaces in the open throat are coated with the protective coating.
摘要翻译：一种处理涡轮机翼片的方法包括在第一和第二涡轮机翼型上沉积保护涂层，以及在沉积之后将第一和第二涡轮机翼型件结合在一起，使得在第一和第二涡轮机翼面之间存在开放的喉部和至少部分表面在开放的喉咙里涂上保护涂层。

6. 发明申请

US20090266446A1 NICKEL BRAZE ALLOY COMPOSITION 有权
标题翻译：镍合金组合物
公开(公告)号：US20090266446A1
公开(公告)日：2009-10-29
申请号：US12109398
申请日：2008-04-25
申请人： Michael Minor , Paul M. Pellet , Michael L. Miller
发明人： Michael Minor , Paul M. Pellet , Michael L. Miller
IPC分类号： B23K35/22
CPC分类号： C22C19/057 , B23K35/304 , B23K2101/001 , C22C1/0433 , C22C19/055 , C22C19/056
摘要： A nickel braze alloy composition includes a blend of a first nickel alloy and a second nickel alloy. The first nickel alloy includes about 4.75 wt %-10.5 wt % of chromium, about 5.5 wt %-6.7 wt % of aluminum, up to about 13 wt % cobalt, about 3.75 wt %-9.0 wt % of tantalum, about 1.3 wt %-2.25 wt % of molybdenum, about 3.0 wt %-6.8 wt % of tungsten, about 2.6 wt %-3.25 wt % of rhenium, up to about 0.02 wt % of boron, about 0.05 wt %-2.0 wt % of hafnium, up to about 0.14 wt % of carbon, up to about 0.35 wt % of zirconium, and a balance of nickel. The second nickel alloy includes about 21.25 wt %-22.75 wt % of chromium, about 5.7 wt %-6.3 wt % of aluminum, about 11.5 wt %-12.5 wt % of cobalt, about 5.7 wt %-6.3 wt % of silicon, boron in an amount no greater than 1.0 wt %, and a balance of nickel.
摘要翻译：镍钎焊合金组合物包括第一镍合金和第二镍合金的共混物。第一种镍合金包括约4.75wt％-10.5wt％的铬，约5.5wt％-6.7wt％的铝，至多约13wt％的钴，约3.75wt％的-9.0wt％的钽，约1.3wt％ -2.25重量％的钼，约3.0重量％的-6.8重量％的钨，约2.6重量％的-3.25重量％的铼，至多约0.02重量％的硼，约0.05重量％〜2.0重量％的铪，至约0.14重量％的碳，至多约0.35重量％的锆，余量为镍。第二镍合金包括约21.25重量％-22.75重量％的铬，约5.7重量％-6.3重量％的铝，约11.5重量％-12.5重量％的钴，约5.7重量％-6.3重量％的硅，硼不大于1.0重量％，余量为镍。

7. 发明授权

US09687926B2 Trailing edge machining of a workpiece 有权
公开(公告)号：US09687926B2
公开(公告)日：2017-06-27
申请号：US12417714
申请日：2009-04-03
申请人： Carl W. Mercier , Daniel E. Quinn , David J. Hiskes , Paul M. Pellet , Michael L. Miller
发明人： Carl W. Mercier , Daniel E. Quinn , David J. Hiskes , Paul M. Pellet , Michael L. Miller
IPC分类号： B23H1/04 , B23H1/00 , B23H9/10 , B23H11/00 , B23Q3/06 , B24B19/14 , B24B41/06
CPC分类号： B23H9/10 , B23H11/003 , B23Q3/063 , B24B19/14 , B24B41/06
摘要： A method of securing an workpiece for machining the trailing edge. The workpiece has a platform from which extends an airfoil, the airfoil including a leading edge and a trailing edge, and a pressure side and a suction side. A fixture with at least one locating datum that relates to the platform and at least one locating datum that relates to the leading edge is provided. The fixture does not contact the trailing edge of the workpiece. The workpiece is positioned so that the platform is against the related locating datum and the leading edge is against the related locating datum. The workpiece is secured within the fixture, and the trailing edge of the workpiece is machined.

8. 发明申请

US20090274562A1 Coated turbine-stage nozzle segments 审中-公开
标题翻译：涂层涡轮级喷嘴段
公开(公告)号：US20090274562A1
公开(公告)日：2009-11-05
申请号：US12151102
申请日：2008-05-02
申请人： Michael J. Minor , Michael L. Miller , Paul M. Pellet
发明人： Michael J. Minor , Michael L. Miller , Paul M. Pellet
IPC分类号： F01D5/14 , B23P6/00
CPC分类号： F01D9/04 , F01D5/288 , Y10T29/49746
摘要： A method for coating a nozzle segment, the method comprising separating an outer shroud and an inner platform of the nozzle segment along pathways that bisect a first stator vane and a second stator vane of the of the nozzle segment, coating the first stator vane and the second stator vane after separating the outer shroud and the inner platform, and rejoining the separated outer shroud and the separated inner platform after coating the first stator vane and the second stator vane.
摘要翻译：一种用于涂覆喷嘴段的方法，所述方法包括沿着将所述喷嘴段的第一定子叶片和第二定子叶片平分的路径分离所述喷嘴段的外护罩和内平台，涂覆所述第一定子叶片和第二定子叶片在分离外护罩和内平台之后，并且在涂覆第一定子叶片和第二定子叶片之后重新接合分离的外护罩和分离的内平台。

9. 发明申请

US20100252533A1 TRAILING EDGE MACHINING OF A WORKPIECE 有权
标题翻译：工作的边缘加工
公开(公告)号：US20100252533A1
公开(公告)日：2010-10-07
申请号：US12417714
申请日：2009-04-03
申请人： Carl W. Mercier , Daniel E. Quinn , David J. Hiskes , Paul M. Pellet , Michael L. Miller
发明人： Carl W. Mercier , Daniel E. Quinn , David J. Hiskes , Paul M. Pellet , Michael L. Miller
IPC分类号： B23H1/04 , B23H1/00
CPC分类号： B23H9/10 , B23H11/003 , B23Q3/063 , B24B19/14 , B24B41/06
摘要： A method of securing an workpiece for machining the trailing edge. The workpiece has a platform from which extends an airfoil, the airfoil including a leading edge and a trailing edge, and a pressure side and a suction side. A fixture with at least one locating datum that relates to the platform and at least one locating datum that relates to the leading edge is provided. The fixture does not contact the trailing edge of the workpiece. The workpiece is positioned so that the platform is against the related locating datum and the leading edge is against the related locating datum. The workpiece is secured within the fixture, and the trailing edge of the workpiece is machined.
摘要翻译：一种固定用于加工后缘的工件的方法。工件具有一个平台，从该平台延伸翼型件，该翼型件包括前缘和后缘，以及压力侧和吸力侧。提供具有至少一个与平台相关的定位基准的固定装置和至少一个与前缘相关的定位基准。夹具不接触工件的后缘。工件被定位成使得平台抵靠相关的定位基准，并且前缘抵靠相关的定位基准。工件被固定在固定装置内，并且加工工件的后缘。

10. 发明申请

US20140272764A1 SPATIAL 3D STERIOSCOPIC INTRAORAL CAMERA SYSTEM BACKGROUND 有权
标题翻译：空间三维立体摄影摄像机系统
公开(公告)号：US20140272764A1
公开(公告)日：2014-09-18
申请号：US13830360
申请日：2013-03-14
申请人： Michael L. Miller , Walt Froloff
发明人： Michael L. Miller , Walt Froloff
IPC分类号： A61B1/06 , A61B5/00 , A61B1/00 , A61B19/00 , A61B1/24 , A61B1/05
CPC分类号： A61B1/0684 , A61B1/00009 , A61B1/00016 , A61B1/0002 , A61B1/00193 , A61B1/051 , A61B1/0638 , A61B1/24 , A61B5/0035 , A61B5/0066 , A61B5/0088 , A61B6/14 , A61B6/5247 , A61B2576/00
摘要： Spatial 3D stereoscopic video is generated with a dual camera subassembly in a hand held device. The 3D Left-Right Multiplexed Spatial Stereoscopic video stream is wirelessly coupled to a processing system for simultaneous visualization comparison with intraoral cavity digital dental impression 3D CAD formatted files, Cone Beam Panoramic Computed Tomography images, Optical Coherence Tomography planar images and Panoramic X-ray image digital files for Stereoscopic visualization on stereoscopic displays and occluding viewing glasses.
摘要翻译：利用手持设备中的双相机子组件生成空间3D立体视频。 3D左右复用空间立体视频流无线耦合到处理系统，用于与口腔内数字牙科印象3D CAD格式文件，锥形全景计算机断层摄影图像，光学相干断层扫描平面图像和全景X射线图像的同时可视化比较用于立体显示和闭塞观看眼镜的立体可视化的数字文件。

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